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US4725708A Expired / Lapsed US ⏱️ 0.0 years remaining

Method for padding a copper type alloy material upon a base of aluminum type metal using laser beam oscillating transversely to its tracking direction

Assignee: Toyota Motor Corp
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Filing: 1986-07-15
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Granted: 1988-02-16
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Expires: 2006-07-15
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Abstract

Abstract In this method for padding, a layer of a copper type alloy material in powdered form is laid upon a portion of a base of aluminum type metal which is to be padded. Then a laser beam, concentrated to a spot from about 0.5 mm to about 2.0 mm in diameter with an output density of from about 80 watt/mm 2 to about 20,000 watt/mm 2 , is irradiated upon this layer of powdered copper type alloy material upon the base of aluminum type metal. The laser beam and the base of aluminum type metal are relatively moved in a relative longitudinal direction at a longitudinal speed of from about 100 mm per minute to about 3000 mm per minute; and they are also reciprocatingly moved in a relative direction substantially transverse to the longitudinal direction at an transverse oscillating frequency of above about 80 Hz. Thereby, good padding efficiency is obtained. The copper type alloy material may initially be applied as a powder including a binder and then be dried, before the laser irradiation; or it may be applied automatically substantially during the laser irradiation.

Inventors

  • 👤 Minoru Kawasaki
  • 👤 Kazuhiko Mori

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 10:54
CPC Classifications
C; C23; C23C; C23C26/00; B; B22; B22F; B22F10/00; B22F10/20; B22F10/28; B22F10/30; B22F10/36; B23; B23K; B23K26/00; B23K26/20; B23K26/32; B23K26/34; B23K35/00; B23K35/22; B23K35/24; B23K35/30; B23K35/302; B29; B29C; B29C64/00; B29C64/10; B29C64/141; B29C64/153; B22F10/32; B22F10/322; B22F12/00; B22F12/40; B22F12/44; B22F12/49; B23K2103/00; B23K2103/08; B23K2103/10; B23K2103/12; B23K2103/18; Y; Y02; Y02P; Y02P10/00; Y02P10/25

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 289 words
A method of improving the resistivity to heat, wearing and corrosion of a surface portion of an aluminum type metal, comprising: laying a layer of copper type alloy to a thickness of at least 0.2 mm on said surface portion of said aluminum type metal; irradiating a laser beam, concentrated to a spot having a diameter of about 0.5 mm to about 5.0 mm and an output density of from about 80 watt/mm 2 to about 20,000 watt/mm 2 upon said layer of powdered copper type alloy, while relatively moving said laser beam and said layer of powdered copper type alloy carried on said surface portion of said aluminum type metal in a relatively longitudinal direction at a longitudinal speed of from about 100 mm per minute to 3000 mm per minute and also relatively reciprocating said laser beam and said layer of powdered copper type alloy carried on said surface portion of said aluminum type metal in a relatively transverse direction substantially perpendicular to said longitudinal direction at an oscillation frequency of about 80 Hz; wherein the rate and dwelling of irradiation of said laser beam at each spot of said layer of powdered copper type alloy carried on said surface portion of said aluminum type metal are so adjusted that each part of said layer of powdered copper type alloy becomes substantially completely molten once with no substatial alloying with said aluminum type metal except at portions of the surface region of said surface portion of said aluminum type metal having a thickness of about 0.05 mm so that said molten layer of powdered copper type alloy forms a pad layer firmly bound to said surface portion of said aluminum type metal along a thin alloyed interface.
Claim 2
Independent Claim 289 words
A method of improving the resistivity to heat, wearing and corrosion of a surface portion of an aluminum type metal, comprising: laying a layer of copper type alloy to a thickness of at least 0.2 mm on said surface portion of said aluminum type metal; irradiating a laser beam, concentrated to a spot having a diameter of about 0.5 mm to about 5.0 mm and an output density of from about 80 watt/mm 2 to about 20,000 watt/mm 2 upon said layer of powdered copper type alloy, while relatively moving said laser beam and said layer of powdered copper type alloy carried on said surface portion of said aluminum type metal in a relatively longitudinal direction at a longitudinal speed of from about 100 mm per minute to 3000 mm per minute and also relatively reciprocating said laser beam and said layer of powdered copper type alloy carried on said surface portion of said aluminum type metal in a relatively transverse direction substantially perpendicular to said longitudinal direction at an oscillation frequency of about 80 Hz; wherein the rate and dwelling of irradiation of said laser beam at each spot of said layer of powdered copper type alloy carried on said surface portion of said aluminum type metal are so adjusted that each part of said layer of powdered copper type alloy becomes substantially completely molten once with no substatial alloying with said aluminum type metal except at portions of the surface region of said surface portion of said aluminum type metal having a thickness of about 0.05 mm so that said molten layer of powdered copper type alloy forms a pad layer firmly bound to said surface portion of said aluminum type metal along a thin alloyed interface.
Claim 3
Dependent Claim 98 words
A method according to claim 1, wherein said aluminum type metal consists of from about 2.0% to about 4.0% CU, from about 5.0% to about 7.0% Si, from about 0.2% to about 0.4% Mg, less than about 0.5% Zn, less than about 0.5% Fe, from about 0.2% to about 0.4% Mn, less than about 0.35% Ni, less than about 0.2% Ti, less than about 0.2% Pb, less than 0.1% Sn, less than 0.2% Cr, and balance substantially Al, and said copper type alloy consists of about 15.0% Ni, about 3.0% Fe, about 1.0% P, and remainder substantially Cu.
Claim 4
Dependent Claim 100 words
A method according to claim 1, wherein said aluminum type metal consists of from about 2.0% to about 4.0% Cu, from about 5.0% to about 7.0% Si, from about 0.2% to about 0.4% Mg, less than about 0.5% Zn, less than about 0.5% Fe, from about 0.2% to about 0.4% Mn, less than about 0.35% Ni, less than about 0.2% Ti, less than about 0.2% Pb, less than about 0.1% Sn, less than about 0.2% Cr, and balance substantially Al, and said copper type alloy consists of about 20.0% Ni, about 4.5% Fe, about 1.0% P, and remainder substantially Cu.

References Cited (Backward Citations)

US4015100A Cited
US3952180A Cited
DE2740569A1 Cited
US4157923A Cited
FR2385810A1 Cited
US4537793A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-02-15 1991-08-17 1992-02-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-02-15 1995-08-17 1996-02-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-02-15 1999-08-17 2000-02-16 $7700.00 Window Closed / Lapsed

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